发明名称 |
WINGLET |
摘要 |
A winglet comprising a tubular main spar with forward and aft main spar webs joined by upper and lower main spar caps; a front spar with a front spar web, an upper front spar cap, and a lower front spar cap; an upper skin joined to the upper main spar cap and the upper front spar cap; and a lower skin joined to the lower main spar cap and the lower front spar cap. The winglet is manufactured by co-curing the upper skin to the upper main spar cap and the upper front spar cap; and co-curing the lower skin to the lower main spar cap and the lower front spar cap. |
申请公布号 |
US2016075429(A1) |
申请公布日期 |
2016.03.17 |
申请号 |
US201414785114 |
申请日期 |
2014.04.17 |
申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
FONG Tony;AXFORD Timothy;CHAUSSEE Julien |
分类号 |
B64C23/06;B32B38/18 |
主分类号 |
B64C23/06 |
代理机构 |
|
代理人 |
|
主权项 |
1. A winglet comprising a tubular main spar with forward and aft main spar webs joined by upper and lower main spar caps; a front spar with a front spar web, an upper front spar cap, and a lower front spar cap; an upper skin joined to the upper main spar cap and the upper front spar cap; and a lower skin joined to the lower main spar cap and the lower front spar cap. |
地址 |
Bristol GB |